List of Effective Pages

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1 List of Effective Pages Page No. Revision No. Revision Date Page No. Revision No. Revision Date IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/ /01/2016

2 List of Effective Pages Page No. Revision No. Revision Date Page No. Revision No. Revision Date IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/ /01/2016

3 List of Effective Pages Page No. Revision No. Revision Date Page No. Revision No. Revision Date IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/2016 IV /01/ /01/2016

4 Outline Airframe Part 2, Systems and Components, Curriculum Instructional Units, Segments and Estimated Instructional Time Aircraft Landing Gear Systems (Meets the requirements of Part 147, Appendix C-Airframe Systems and Components-A) 29. Inspect, check, service, and repair landing gear, retraction systems, shock struts, brakes, wheels, tires, and steering systems Ref: 147-C-A hrs Level 3 A. Clean and store tires Level 2 B. Inspect, demount, repair and reinstall tires on wheels Level 3 C. Remove, inspect, service and reinstall a wheel assembly on an axle Level 3 D. Disassemble, identify components and reassemble mechanical and hydraulic type brake assemblies Level 2 E. Replace a brake actuating cylinder Level 3 F. Adjust clearance on show, multiple disk and single disc brake Level 3 G. Inspect, repair and operationally check a master cylinder Level 3 H. Inspect, service and describe the operation of power brake and emergency brake systems Level 2 I. Recognize probable cause of brake malfunctions Level 2 J. Bleed air from hydraulic brake systems Level 3 K. Service, repair and troubleshoot landing gear oleo struts Level 2 L. Describe the operation of an oleo shock strut Level 2 M. Operate, inspect and adjust a retractable landing gear Level 3 IV /01/ /01/2016

5 N. Check landing gear alignment Level 2 O. Inspect, adjust and service nose and tail wheel steering and damping mechanisms Level 3 Estimated Instructional Time: 82.0 hrs Hydraulic and Pneumatic Power Systems (Meets the requirements of Part 147, Appendix C-Airframe Systems and Components-B) 30. Repair hydraulic and pneumatic power systems components Ref: 147-C-B hrs Level 3 A. Select and install seals Level 2 B. Identify, remove and install a hydraulic selector valve Level 2 C. Remove and install pressure regulators Level Identify and select hydraulic fluids Ref: 147-C-B hrs Level 3 A. Indentify and select hydraulic fluids Level Inspect, check, service, troubleshoot, and repair hydraulic and pneumatic power systems Ref: 147-C-B hrs Level 3 A. Solve problems involving force, area and pressure Level 2 B. Interpret reference information pertaining to operation of a basic hydraulic system Level 2 C. Compare constant pressure and open center types of hydraulic systems Level 2 D. Inspect and service hydraulic reservoirs Level 3 E. Identify and describe the operation of constant and variable displacement hydraulic pumps Level 2 F. Check, inspect, remove and install hydraulic power pumps Level 3 IV /01/ /01/2016

6 G. Troubleshoot hydraulic pumps Level 3 H. Remove, install, inspect, service and check hydraulic accumulator Level 3 I. Troubleshoot and determine the cause of low, high or fluctuating system hydraulic pressure Level 3 J. Inspect, check and service a hydraulically operated flap system Level 2 Estimated Instructional Time: 72.0 hrs Cabin Atmosphere Control Systems (Meets the requirements of Part 147, Appendix C-Airframe Systems and Components-C) 33. Inspect, check, troubleshoot, service, and repair heating, cooling, air conditioning, pressurization systems, and air cycle machines Ref: 147-C-C hrs Level 1 A. The inspection, checking and troubleshooting of aircraft combustion heaters and exhaust type heat exchangers Level 1 B. The checking and troubleshooting of aircraft vapor cycle and air cycle cooling systems Level 1 C. The functions and principles of operation of aircraft air conditioning Level 1 D. The principles of operations and control of cabin pressurizations Level Inspect, check, troubleshoot, service, and repair heating, cooling, air conditioning, and pressurization systems Ref: 147-C-C hrs Level 1 A. Identify components of an aircraft combustion heater, Freon cooling system, and an air cycle expansion turbine Level 1 B. Repair or replacement procedures for air conditioning and pressurization components Level 1 IV /01/ /01/2016

7 C. Repair or replacement procedures for aircraft oxygen system components Level Inspect, check, troubleshoot, service, and repair oxygen systems Ref: 147-C-C hrs Level 2 A. Inspect, check and service oxygen systems Level 2 Estimated Instructional Time: 30.0 hrs Aircraft Instrument Systems (Meets the requirements of Part 147, Appendix C-Airframe Systems and Components-D) 36. Inspect, check, service, troubleshoot, and repair electronic flight instrument systems and both mechanical and electrical heading, speed, altitude, temperature, pressure, and position indicating systems to include the use of built-in test equipment Ref: 147-C-D hrs Level 1 A. Inspect, check, service, troubleshoot and repair instrument systems Level Install instruments and perform a static pressure system leak test Ref: 147-C-D hrs Level 2 A. Handling and storing of instruments Level 2 B. Install instrument panel and instruments Level 2 Estimated Instructional Time: 20.0 hrs IV /01/ /01/2016

8 Communication and Navigation Systems (Meets the requirements of Part 147, Appendix C-Airframe Systems and Components-E) 38. Inspect, check, and troubleshoot autopilot, servos, and approach coupling systems Ref: 147-C-E hrs Level 1 A. Purpose and operating principles of autopilots and approach control systems Level Inspect, check, and service aircraft electronic communication and navigation systems, including VHF passenger address interphones and static discharge devices, aircraft VOR, ILS, LORAN, Radar beacon transponders, flight management computers, and GPWS Ref: 147-C-E hrs Level 1 A. Types and installation of aircraft electronic communications and navigation equipment Level 1 B. FCC regulations pertaining to two-way radio operation Level Inspect and repair antenna and electronic equipment installations Ref: 147-C-E hrs Level 2 A. Repair and replace aircraft antennas and related electronic equipment Level 2 B. Identify and describe purpose of static discharges Level 2 Estimated Instructional Time: 20.0 hrs Aircraft Fuel Systems (Meets the requirements of Part 147, Appendix C-Airframe Systems and Components-F) 41. Check and service fuel dump systems Ref: 147-C-F hrs Level 1 A. Describe the checking and servicing of a fuel dump system Level 1 IV /01/ /01/2016

9 42. Perform fuel management transfer and defueling Ref: 147-C-F hrs Level 1 A. Perform fuel transfer and defueling Level Inspect, check, and repair pressure fueling systems Ref: 147-C-F hrs Level 1 A. Describe the inspection, checking and repair of pressure fueling systems Level Repair aircraft fuel system components Ref: 147-C-F hrs Level 2 A. Interpret information pertaining to repair of fuel system components Level Inspect and repair fluid quantity indicating systems Ref: 147-C-F hrs Level 2 A. Inspect and troubleshoot fuel quantity indication systems Level Troubleshoot, service, and repair fluid pressure and temperature warning systems Ref: 147-C-F hrs Level 2 A. Troubleshoot, service, and repair fuel pressure and temperature warning systems Level Inspect, check, service, troubleshoot, and repair aircraft fuel systems Ref: 147-C-F hrs Level 3 A. Inspect and service, fuel tanks Level 3 B. Inspect, check, service, troubleshoot and repair fuel valves and fuel pumps Level 3 Estimated Instructional Time: 36.0 hrs IV /01/ /01/2016

10 Aircraft Electrical Systems (Meets the requirements of Part 147, Appendix C-Airframe Systems and Components-G) 48. Repair and inspect aircraft electrical system components, crimp and splice wiring to manufacturers specifications, and repair pins and sockets of aircraft connectors Ref: 147-C-G hrs Level 2 A. Determine causes and effects of switch chatter in solenoid switches and relays Level 2 B. Inspect installation and check circuits and anti-collision and positions lights Level 2 C. Inspect, check, and repair landing and taxi light installations Level 2 D. Inspect, check, service and repair aircraft interior lighting installations Level 2 E. Inspect, check, service and repair cockpit lights and lighting circuits Level 2 F. Inspect and check electrical equipment installations for integrity of mounting and connections Level 2 G. Inspect, check, and repair passenger call system Level 1 H. Locate replacement procedures and parts numbers for electrical component replacements Level Install, check, and service airframe electrical wiring, controls, switches, indicators, and protective devices Ref: 147-C-G hrs Level 3 A. Types and characteristics of aircraft fuses, circuit breakers and switches Level 1 B. Select and install aircraft electrical switches and wiring to components Level 3 C. Installation requirements and characteristics for aircraft electrical wiring systems and junction boxes Level 2 D. Install electrical terminals, splices and bonding jumpers Level 3 E. Install aircraft electrical wiring in a conduit Level 2 IV /01/ /01/2016

11 F. Check and connect quick-disconnect plugs and receptacles Level 2 G. Protect electrical emergency switches against accidental actuation Level 3 H. Identify and describe characteristics of aircraft high tension and low tension electrical wiring Level (a) Inspect, check, troubleshoot, service, and repair alternating and direct current electrical systems Ref: 147-C-G hrs Level 3 (b) Inspect, check, and troubleshoot constant speed and integrated speed drive generators Ref: 147-C-G hrs Level 1 A. Methods of controlling output current and voltage of compound DC generators Level 2 B. Check, troubleshoot and repair an aircraft dual DC generator electrical system Level 3 C. Methods of providing AC in aircraft having only DC electrical systems Level 1 D. Troubleshoot and repair a DC electrical system supplied by an alternator Level 3 E. Characteristics and advantages of AC aircraft electrical systems Level 1 F. Identify components and operating elements of a 208/114 volt AC aircraft electrical system Level 2 G. Inspect, check and troubleshoot constant speed and integrated speed drive generators Level 1 Estimated Instructional Time: hrs IV /01/ /01/2016

12 Position and Warning Systems (Meets the requirements of Part 147, Appendix C-Airframe Systems and Components-H) 51. Inspect, check, and service speed and configuration warning systems, electrical brake controls, and antiskid systems Ref: 147-C-H51 11 hrs Level 2 A. Principles of operation, inspection and check of speed, stall, takeoff warning systems and antiskid brake control systems Level 1 B. Show simulated operation of antiskid takeoff warning systems Level Inspect, check, troubleshoot, and service landing gear position indicating and warning systems Ref: 147-C-H52 9 hrs Level 3 A. Inspect, check, troubleshoot, service and repair landing gear position indicating and warning systems Level 3 Estimated Instructional Time: 20.0 hrs Ice and Rain Control Systems (Meets the requirements of Part 147, Appendix C-Airframe Systems and Components-I) 53. Inspect, check, troubleshoot, service and repair airframe ice and rain control system Ref: 147-C-I53 12 hrs Level 2 A. Principles of installation, operation and checking deicing and anti-icing systems Level 1 B. Replace inspect and check operation of electrically operated air scoop and pitot static or static vent anti-icing Level 2 Estimated Instructional Time: 12.0 hrs IV /01/ /01/2016

13 Fire Protection Systems (Meets the requirements of Part 147, Appendix C-Airframe Systems and Components-J) 54. Inspect, check, service smoke and carbon monoxide detection systems Ref: 147-C-J54 1 hrs Level 1 A. Principles of operation of smoke and carbon monoxide detectors Level Inspect, check, service, troubleshoot, and repair aircraft fire detection and extinguishing systems Ref: 147-C-J55 11 hrs Level 3 A. Inspect, check, troubleshoot and repair fire detection systems Level 3 B. Select and operate fire extinguishers Level 2 C. Check, troubleshoot and repair built-in fire extinguishing systems Level 2 Estimated Instructional Time: 12.0 hrs Additional Practice and/or Examinations Grand Total Airframe Part 2, Systems and Components, Curriculum 5.0 hrs hrs IV /01/ /01/2016

14 Outline Airframe Part 2, Systems and Components, Curriculum Detail Aircraft Landing Gear Systems (Meets the requirements of Part 147, Appendix C-Airframe Systems and Components-A) 29. Inspect, check, service, and repair landing gear, retraction systems, shock struts, brakes, wheels, tires, and steering systems (EIT = 82 hrs, T = 32 hrs, L/S = 50 hrs) Level 3 A. Clean and store tires Level 2 Used aircraft tires, approved tire cleaning materials and appropriate written information describing the cleaning and storing of tires. The student will clean an aircraft the, removing oils and other deteriorating materials and describe the procedure to be followed when storing tires and other rubber aircraft products. The cleaning and description of procedure will comply with the reference information without error or omission. B. Inspect, demount, repair and reinstall tires on wheels Level 3 Aircraft wheels with tires of both the tube and tubeless types, written procedures for tire servicing. AC or equivalent publications and appropriate tire servicing tools and equipment. IV /01/ /01/2016

15 The student will demount one tubeless tire and one tube type tire from the wheel. He will inspect the tires, tube and wheel assembly, determine the necessary repairs, make one repair to a tube, reinstall the tire and tube and inflate to correct pressures. He will practice and explain the' safety precautions related to tire servicing Written procedures will be followed without error. One completed tire installation will conform to return-to-service standards. C. Remove, inspect, service and reinstall a wheel assembly on an axle Level 3 An aircraft wheel assembly mounted on an airplane or on a mock-up, appropriate written service information and wheel removal tools and equipment. The student will raise the aircraft and re- move the wheel from the axle. He/She will inspect the wheel assembly and bearings and prepare a written list of five discrepancies that are commonly found. He will describe the reasons for rejecting wheel components and describe the repairs that may be accomplished. He will lubricate the bearings of the wheel assembly, reinstall the wheel on the axle, adjust the bearing play, and lower the airplane. Service information and procedure will be followed without error or omission. Correct nomenclature will be used as a part of the descriptions and explanations. The task will be accomplished at a return-to-service standard. IV /01/ /01/2016

16 D. Disassemble, identify components and reassemble mechanical and hydraulic type brake assemblies Level 2 Typical shoe type mechanically operated aircraft brakes; samples of hydraulically actuated brakes of the servo, expander-tube, single and multiple disc types: drawings or diagrams of each type of brake, written service information that identifies the components and describes the operation of the system. The student will disassemble, identify the components, describe the operation and reassemble each brake assembly. Brake assemblies need not meet return-to-service standards. Disassembly, inspection and reassembly operations will be in complete accordance with the service Information pro- vided. Correct nomenclature and terminology will be used throughout the descriptions of operations of the systems. E. Replace a brake actuating cylinder Level 3 An operational hydraulic brake system in stalled in an airplane or mock-up, a spare operational actuating cylinder to replace a wheel cylinder installed in the system, written service Information, appropriate hydraulic fluids and tools. The student will replace an actuating cylinder in the wheel brake assembly; following form a functional test of the system following the replacement of the cylinder. The system will operate normally. There will be no indications of external or Internal leakage. IV /01/ /01/2016

17 F. Adjust clearance on show, multiple disk and single disc brake Level 3 A mock-up or training device that incorporates a wheel and brake assembly of a shoe, multiple-disc and single-^disc types, replacement lining blocks, written service in«formation or manuals and appropriate tools. The student will remove the wheel from the axle, inspect the brake assembly, adjust the clearance of each brake, as necessary, and reinstall the wheel. The adjusted brake (shoe, multiple and single disc) will comply with the clearance adjustments specified in the service information. The procedures and work accomplished will be of return-to-service standard. G. Inspect, repair and operationally check a master cylinder Level 3 An operational brake master cylinder, written service information and overhaul manuals, required seals, gaskets, fluids and suitable equipment to check the operation of a master cylinder. The student will disassemble a brake master cylinder, inspect the components, replace seals (as required), reassemble and check the operation of the master cylinder. Procedures will be in accordance with the written information. The reassembled cylinder will operate without internal or external leakage. H. Inspect, service and describe the operation of power brake and emergency brake systems Level 2 IV /01/ /01/2016

18 An operational power brake system incorporating a power brake control valve, shuttle valve and brake assembly, a brake subsystem, accumulator, an emergency brake power system, debooster, hydraulic fuse and anti-skid device, a diagram or drawing of the entire system and written information describing the operation and servicing of the system. The student will identify the components of the system and label the diagram or drawing. Using the reference information, he will service and operate the system. He/She will describe the operation of power brake and emergency brake systems. Correct nomenclature and terminology will be used to describe the system operation and to label the diagram. Operation and servicing of the system will be in accordance with the reference information. I. Recognize probable cause of brake malfunctions Level 2 The airplane manufacturer's service information, ten written statements describing brake fading, excessive pedal travel, grabbing brakes, spongy brake action and dragging and locked brakes. The student will describe the probable cause for each of the malfunctions described in written statements. The student will provide at least one probable cause for each of the malfunctions. Information obtained from the manufacturer's service manual will be interpreted without error. J. Bleed air from hydraulic brake systems Level 3 IV /01/ /01/2016

19 Manufacturer's service instruction, appropriate bleeding equipment, supply of hydraulic fluids, and an operable hydraulic system into which air has been introduced. The student will bleed the system of air. The procedure specified in the service instructions will be followed without error or omission. The system, following bleeding, will be completely operational. K. Service, repair and troubleshoot landing gear oleo struts Level 2 A completely assembled and operational shock strut (installed on an airplane or mock-up), the airplane manufacturer's service information, replacement high-pressure air valves and seals, hydraulic fluid, and appropriate tools and equipment to disassemble and inflate shock struts. The student will deflate a shock strut, drain the fluid, remove the piston from the cylinder, install seals, reassemble the strut, service with fluid, reinstall the air valve and inflate the strut. He will locate and interpret information from the service instructions and explain the probable causes of faults normally encountered in the operation of struts. The servicing procedures will be followed without deviation. The shock strut following service and repair will meet return to flight standards. The service information pertaining to troubleshooting the strut will be interpreted without error. L. Describe the operation of an oleo shock strut Level 2 IV /01/ /01/2016

20 Shock struts of the air-oil and spring-oil types, drawings of each type of strut and the manufacturer's service instructions; a matching type ten question examination pertaining to shock struts. The student will identify and label the components of each type of shock strut, explain the purpose of shock struts and describe the operation of both types of struts. Correct nomenclature will be used when labeling the drawings and describing the operation of the shock struts. Manufacturer's service information will be interpreted without error or omissions. M. Operate, inspect and adjust a retractable landing gear Level 3 An operational retractable landing gear (installed in an airplane or mock-up), written information or the manufacturer's service manual, an appropriate power source to permit operation of the gear, special tools and lubrication equipment as specified in the service information, mirrors, lights, measuring devices, etc. The student will operate the retractable landing gear, inspect and adjust the landing gear to meet return-to-service standards. The components of the landing gear need not be airworthy, but the adjustments and procedures outlined in the service manual will be followed within return-to-service limits. N. Check landing gear alignment Level 2 IV /01/ /01/2016

21 An aircraft incorporating either a fixed or retractable landing gear, the airframe manufacturer's service information necessary to check landing gear alignment and the necessary measuring and alignment tools and equipment. The student will measure and record the caster, camber, toe-in and toe-out of the landing gear. Within the tolerance specified in the service information, he will judge whether the landing gear is accept-able for return-to-flight. If the alignment of the landing gear is unacceptable, he will interpret the service information and recommend the method that would return the gear alignment to acceptable limits. Service information will be correctly interpreted and procedure for measuring gear alignment will be followed without error. O. Inspect, adjust and service nose and tail wheel steering and damping mechanisms Level 3 An airplane or mock-up incorporating an operational nose wheel steering and dampener; an airplane or mock-up incorporating an operational tail wheel and shimmy dampener; the manufacturer's servicing information, tools and hydraulic fluids. The student will inspect, adjust and service both nose and tail wheel steering and damping mechanisms. Service information will be correctly interpreted. After servicing and adjusting the steering and damping mechanism will function as specified in the manufacturer manual. IV /01/ /01/2016

22 Hydraulic and Pneumatic Power Systems (Meets the requirements of Part 147, Appendix C-Airframe Systems and Components-B) 30. Repair hydraulic and pneumatic power systems components (EIT = 15 hrs, T = 7 hrs, L/S = 8 hrs) Level 3 A. Select and install seals Level 2 Hydraulic components not requiring, complex assembly, disassembly, (i.e., master and wheel brake cylinders, actuating cylinders, etc.) various types and sizes of seals and fluids, reference information describing the procedure for replacing and testing seals in a hydraulic unit and a means for testing the following seal replacement. The student will use and interpret information that will assist in identifying and selecting seals for use in ester, petroleum and vegetable base hydraulic fluids. He will install seals in one unit in accordance with the procedures specified in the manual and test the unit following reassembly. The unit which has had the seals replaced will function as it was designed to operate and will be free of both external and internal leaks. B. Identify, remove and install a hydraulic selector valve Level 2 An operational hydraulic system or a segment including at least a source of hydraulic pressure, a selector valve and actuating cylinder, written service instructions, a spare selector valve for installation into the system, line cap-plugs and a supply of hydraulic fluid. IV /01/ /01/2016

23 The student will identify, remove and install a selector valve into the system. He/She will operationally check the system following placement of the selector valve. The selector valve will be identified regardless of the type of valve. The removal and Installation procedures will he adhered to without error or omission. The system will function as it was designed to operate. C. Remove and install pressure regulators Level 2 Operational hydraulic system, written reference information, a replacement pressure regulator, line cap-plugs and a supply of hydraulic fluid. The student will identify, remove and install a pressure regulator in the hydraulic system. He will test the system following installation of the regulator land adjust the pressure of the system. The procedures will he fully in accordance with the written instructions. The pressure will be adjusted within the tolerance specified in the instructions. 31. Identify and select hydraulic fluids (EIT = 2 hrs, T = 1 hr, L/S = 1 hr) Level 3 A. Indentify and select hydraulic fluids Level 3 Samples of ester-base, petroleum-base and vegetable- base hydraulic fluids; sample placards of the type used or attached to hydraulic reservoirs; written reference information describing the characteristics and identifying features of hydraulic fluids. IV /01/ /01/2016

24 The student will distinguish between the sample fluids by color, odor and specification number. When shown the sample placard or reservoir data plate, he/she will select the fluid that would be used to service the system. He/she will describe the characteristics of each type of hydraulic fluid. The three types of fluids will be identified without error. Reference information and placards will be correctly identified. Correct nomenclature will be used when describing the characteristics of the fluid. 32. Inspect, check, service, troubleshoot, and repair hydraulic and pneumatic power systems (EIT = 55 hrs, T = 25 hrs, L/S = 30 hrs) Level 3 A. Solve problems involving force, area and pressure Level 2 Ten problems (sketches, drawings or narrative), illustrating the relationship of applied force, area of cylinder or piston and pressure per unit area. The student will solve the problems when one of the factors is unknown or the values have been changed. He/She will explain the hydraulic principles involved in the solution of the problem. Bight of the ten problems will be correctly solved. Correct nomenclature and terminology will be used throughout the explanations. B. Interpret reference information pertaining to operation of a basic hydraulic system Level 2 IV /01/ /01/2016

25 Reference manuals, drawings, diagrams, mock-ups, or components installed in an aircraft system, including but not limited to: reservoir pumps, actuating cylinders, check valves, elector valves, relief valves, regulators, accumulators, fuse, flap overload valve, sequence valve, cross-flow valve, shuttle valve and pressure gauges. The student will interpret the reference in- formation and diagram a basic hydraulic system. He/She will show and explain the relationship, purpose and function of each component in the system. Reference information will be interpreted without errors. Correct nomenclature and terminology will be part of all explanations and descriptions. C. Compare constant pressure and open center types of hydraulic systems Level 2 Charts, manuals, mock-ups or complete aircraft hydraulic systems of the constant pressure and the open center types. The student will identify each type of system and compare the components and the means of system pressure regulation. The reference information will be interpreted and comparison made without error. All explanations and descriptions of operation will include use of correct nomenclature and terminology. D. Inspect and service hydraulic reservoirs Level 3 IV /01/ /01/2016

26 An operational hydraulic system or mock-up Provided with a vented or a pressurized reservoir; a supply of hydraulic fluids and written inspection and service instructions applicable to the specific system. The student will inspect and service the reservoir with fluid and check the filter for contamination. The inspection and servicing procedure will be fully in accordance with the servicing instructions. E. Identify and describe the operation of constant and variable displacement hydraulic pumps Level 2 Visual aids manuals and a sample or cutaway of a constant and variable displacement type hydraulic power pump. The student will Identify and describe the operation of one pump of each type. Reference Information will be correctly interpreted. Correct nomenclature will be used when identifying and describing pump operation. F. Check, inspect, remove and install hydraulic power pumps Level 3 IV /01/ /01/2016

27 An operational hydraulic system installed, in an aircraft or on a mock-up; three engine driven Hydraulic pumps, at least one of which has a worn or sheared drive shaft; a suitable accessory drive pad and written instructions describing the inspection, installation and removal of the hydraulic pump. The student will inspect the pump drive shafts and identify the pump with the defective shaft. He will remove and install a pump on the accessory drive pad and check operation of the system, following pump installation. The pump with the defective shaft will be identified without error. Reference information will be correctly interpreted. Removal, installation and checking will be in accordance with the written procedures. G. Troubleshoot hydraulic pumps Level 3 An operational hydraulic system that may be supplied with pressure from an auxiliary power source and written service information. The student will troubleshoot the hydraulic system after the instructor has introduced air into the pump. The student will prime the pump and purge air from the system. The procedures will be in accordance with the reference information. The pump and system, will operate as specified following correction of the fault. H. Remove, install, inspect, service and check hydraulic accumulator Level 3 IV /01/ /01/2016

28 An operational constant pressure hydraulic system Including one at least a power supply pump, pressure Regulating devices, accumulators, flow control valves, Actuators and the manufacturers publication applicable To the specific system. The student will remove, inspect and install an accumulator in the system, he/she will charge the accumulator with air or nitrogen and check the operation of the 'system. He/She will replace high-pressure air valve assemblies as necessary. All tasks will be accomplished in accordance with the manufacturer's maintenance instructions. The system will, following servicing, comply with all operational specifications established in the written service instructions. I. Troubleshoot and determine the cause of low, high or fluctuating system hydraulic pressure Level 3 An operational hydraulic system including at least a power supply pump, pressure-regulating devices, accumulators, flow control valves, actuators and the manufacturer's publications applicable to the specific system. The student will operate the system, compare the operating characteristics with the reference information, and detect low, high or fluctuating pressures when faults are introduced into the system by the instructor. He/She will interpret information from the service publications and describe the probable cause for the observed malfunction. He/She will make necessary adjustments to restore the system to operating tolerances. Operation, adjustments and analysis of faults will be in accordance with the written reference information. Following observance and analysis of faults, the system will be restored to operating tolerances specified in the instructions. IV /01/ /01/2016

29 J. Inspect, check and service a hydraulically operated flap system Level 2 An operational hydraulic flap system installed in the aircraft or on a mock-up, and the manufacturer's maintenance and service publications or written reference material. The student will inspect, check and service the flap system. The tasks will be accomplished in accordance with the written instructions and will result in a system that operates within the tolerances specified in the instructions. Cabin Atmosphere Control Systems (Meets the requirements of Part 147, Appendix C-Airframe Systems and Components-C) 33. Inspect, check, troubleshoot, service, and repair heating, cooling, air conditioning, pressurization systems, and air cycle machines (EIT = 14 hrs, T = 14 hrs, L/S = 0 hrs) Level 1 A. The inspection, checking and troubleshooting of aircraft combustion heaters and exhaust type heat exchangers Level 1 Written information, schematic diagrams and questions with multiple-choice answers concerning aircraft cabin pressurization. The student will select answers for 14 questions concerning the basic principles of cabin pressurization and how it is controlled, the relationships of cabin pressure to ambient pressure during a flight, the purposes and operation of check valves in delivery air ducts, outflow valves, emergency relief valves, and negative pressure relief valves. IV /01/ /01/2016

30 Select correct answers for at least ten questions. B. The checking and troubleshooting of aircraft vapor cycle and air cycle cooling systems Level 1 Written information and diagrams of an aircraft air conditioning system. The student will write a brief description of the functions of each of the following components in an air conditioning system: the supercharger or compressors the mixing valve, the intercooler or primary heat exchanger, the passenger's cold air distribution system cabin and duct sensors, ambient air sensor, main distribution ducts, cabin air inlet louvers, cabin air exhaust outlets, outflow valve, recirculation fan, and ground blower. At least eight descriptions will be in accordance with information provided. C. The functions and principles of operation of aircraft air conditioning Level 1 Written information and questions with multiple-choice answers concerning aircraft surface combustion heaters and exhausttype heat exchangers. The student will select answers for ten questions with regard to surface combustion heater operating principles and shooting, exhaust-type heat exchanger operation and troubleshooting, inspection requirements of cabin heating systems. Select correct answers for at least seven questions. IV /01/ /01/2016

31 D. The principles of operations and control of cabin pressurizations Level 1 Written information, unlabeled diagrams, and completion type essay statements relative to aircraft vapor-cycle and air-cycle cooling systems. The student will inspect labels in spaces provided to identify components in diagrams of a Freon vapor- cycle aircraft refrigeration system and an air-cycle aircraft cooling system. He will complete essay statements concerning Freon system components, air- cycle machine components, and checking, troubleshooting and servicing aircraft cooling systems. Correct labels and completion words for at least 70 percent of the spaces provided. 34. Inspect, check, troubleshoot, service, and repair heating, cooling, air conditioning, and pressurization systems (EIT = 9 hrs, T = 9 hrs, L/S = 0 hrs) Level 1 A. Identify components of an aircraft combustion heater, Freon cooling system, and an air cycle expansion turbine Level 1 Written information, unlabeled cut-away drawings, and questions with multiple-choice answers. IV /01/ /01/2016

32 The student will identify and label the following items in a cutaway drawing of a surface combustion heater: fuel and combustion air inlets, ventilating air inlet and outlet, exhaust, fuel nozzle, spark plug, overheat and drop-out thermal switches; and show flow patterns by arrows. He will identify and label the major components of a Freon vapor-cycle cooling system. He will identify and label the following items in an air-cycle cooling system: turbine air intake and outlet, turbine, axial flow fan, fan air intake and outlet, oil reservoir, bearing and oil wick, primary and secondary heat exchangers, and show air routings through the turbine, heat exchangers and fan outlet section. Correct labels and arrows for at least 70 percent of the specified items. B. Repair or replacement procedures for air conditioning and pressurization components Level 1 Manufacturer s service manuals or equivalent written material and samples or drawings of air condition and pressurization system components. The student will identify samples or drawings of the following components and list reference page numbers for repair or replacement information for ten of the components identified: cabin supercharger or compressor, air delivery duct check valve, cabin air mixing valve and its actuator, cabin temperature control unit and instruments, outflow valve, and actuator, pressure control unit and instruments, automatic and manual emergency relief valves, cabin ground blower, recirculation fan, and cabin vacuum (negative pressure) relief valve. Correctly identify at least ten components and list correct reference page numbers for repair or replacement information for at least 7 components. IV /01/ /01/2016

33 C. Repair or replacement procedures for aircraft oxygen system components Level 1 Manufacturer's service manuals, AC , or equivalent publications, samples or drawings of oxygen system components and multiple choice questions. The student will select answers to ten questions dealing with repair or replacement of oxygen system components, including oxygen high pressure bottles and regulators, walk around oxygen bottles and regulators, flight crew oxygen masks and flow regulators, passenger oxygen masks and therapeutic oxygen equipment. Select 8 correct answers. 35. Inspect, check, troubleshoot, service, and repair oxygen systems (EIT = 7 hrs, T = 3 hrs, L/S = 4. hrs) Level 2 A. Inspect, check and service oxygen systems Level 2 Manufacturer's service manual or equivalent written information, check sheet or work card, an aircraft or mock-up with an operative oxygen system. The student will check the oxygen system for leakage, check bottle pressure and replace a high-pressure oxygen bottle, check oxygen system pressure, inspect masks for contamination and check an oxygen mask and regulator for proper operation. All Performance will be in compliance with the check sheet or work card provided. IV /01/ /01/2016

34 Aircraft Instrument Systems (Meets the requirements of Part 147, Appendix C-Airframe Systems and Components-D) 36. Inspect, check, service, troubleshoot, and repair electronic flight instrument systems and both mechanical and electrical heading, speed, altitude, temperature, pressure, and position indicating systems to include the use of built-in test equipment (EIT = 9 hrs, T = 4 hrs, L/S = 5 hrs) Level 1 A. Inspect, check, service, troubleshoot and repair instrument systems Level 1 Manufacturer's service manuals or diagrams and written descriptions of a compass system, airspeed/altitude/rate of climb system, gyro attitude systems, temperature/ pressure/ positioning systems, appropriate operational instrument systems mounted in an airplane or mock-up. The student will inspect, check, service, troubleshoot and repair one system, which has been made faulty by an action of the instructor. The student will interpret the written information, correctly identify and correct the fault in the system. 37. Install instruments and perform a static pressure system leak test (EIT = 11 hrs, T = 5 hrs, L/S = 6 hrs) Level 2 A. Handling and storing of instruments Level 2 A random display of aircraft instruments, including direct pressure indicating instruments, gyro instruments, temperature indicating instruments, compasses, and remote indicating indicators and transmitters; suitable cartons or storage containers, sealing plugs and shock absorbing shipping materials. IV /01/ /01/2016

35 The student will remove at least three instruments from the display panel or mock-up, seal all openings to the instrument, attach an identification tag and prepare the instrument for storage or shipment. The task of removing and identifying and preparing the instrument for storage or shipment will demonstrate precautions that will prevent further damage to the instrument. B. Install instrument panel and instruments Level 2 An airplane or mock-up provided with mounting brackets, an instrument panel, with instruments installed, appropriate panel shock mounts; written reference information describing the number, type, and load rating and procedure for installing the shock mounts and panel. The student will install the shock mounts, panel and instruments into the airplane or mock-up. The panel and instruments need not meet return-to- flight standards, but the installation of mounts; panel and instruments will fully comply with the written installation instructions. Communication and Navigation Systems (Meets the requirements of Part 147, Appendix C-Airframe Systems and Components-E) 38. Inspect, check, and troubleshoot autopilot, servos, and approach coupling systems (EIT = 5 hrs, T = 5 hrs, L/S = 0 hrs) Level 1 A. Purpose and operating principles of autopilots and approach control systems Level 1 IV /01/ /01/2016

36 Manufacturer's manuals, written information, and multiple completion essay statements. The student will complete 14 essay statements, by supplying missing words, concerning the purposes and operation of an autopilot, the operating principles of the sensing devices used to provide heading, attitude, and altitude information to the autopilot, the purpose and operation of servos or servomotors, the function of position transmitters and trim indicators, and the purpose and operation of an approach control system. Correctly complete 10 essay statements. 39. Inspect, check, and service aircraft electronic communication and navigation systems, including VHF passenger address interphones and static discharge devices, aircraft VOR, ILS, LORAN, Radar beacon transponders, flight management computers, and GPWS (EIT = 5 hrs, T = 5 hrs, L/S = 0 hrs) Level 1 A. Types and installation of aircraft electronic communications and navigation equipment Level 1 AC &2 or equivalent published information, and questions with multiple-choice answers. The student will select answers for 20 questions concerning electronic communications and navigation systems. The questions will deal with types of equipment used in various aircraft, where and how the equipment is mounted, cooling, and reduction of electrical reference. Select at least 14 correct answers. IV /01/ /01/2016

37 B. FCC regulations pertaining to two-way radio operation Level 1 FCC regulations pertaining to aircraft radio operation, or an equivalent publication and questions concerning 'these regulations. The student will write answers to 10 questions concerning the operation of aircraft and ground radio transmitters, FCC regulations pertaining to radio transmissions acceptable practices and vocabulary usage, proper recognition and acknowledgement techniques and rules covering display of licenses. Correct answers for at least 7 questions. 40. Inspect and repair antenna and electronic equipment installations (EIT - 10 hrs, T = 5 hrs, L/S = 5 hrs) Level 2 A. Repair and replace aircraft antennas and related electronic equipment Level 2 Manufacturer's manuals, AC , AC A, AC or equivalent publications, an aircraft or mock-up with electronic installations which use fixed wire, blade or whip, and flush mounted antennas, and questions with multiple choice answers pertaining to PAR procedures after major repair or alteration has been accomplished. IV /01/ /01/2016

38 The student will locate repair and replacement information for a fixed wire antenna, a blade or whip antenna, and a flush type antenna. Using this information, he will replace one antenna and related electronic Equipment and repair one other antenna, which has been intentionally damaged by the instructor, He will select answers to 6 questions pertaining to PAR requirements for returning an aircraft to service after a radio installation has been made in accordance with approved data. Locate proper information and perform replacement and repairs in accordance with published procedures and specifications for return-to-flight. Select correct answers for at least 5 questions. B. Identify and describe purpose of static discharges Level 2 Written information, AC (or equivalent publication) sample static dischargers on an aircraft or mock-up and drawings of static dischargers which include carbon impregnated braid types, metallic braid types, null-field types, and an ohmmeter. The student will identify each of the three types of static dischargers and write a brief description of how each type performs its intended function. He will also describe how each type is to be inspected and what wear or damage indications require repairs or Replacement and then will inspect the mounting and test the epoxy bond resistance. At least two identifications, two descriptions of functions and two descriptions of repair procedures will be correct, in accordance with information provided. IV /01/ /01/2016

39 Aircraft Fuel Systems (Meets the requirements of Part 147, Appendix C-Airframe Systems and Components-F) 41. Check and service fuel dump systems (EIT = 1 hr, T = 1 hr, L/S = 0 hrs) Level 1 A. Describe the checking and servicing of a fuel dump system Level 1 Visual aids and the technical data available from the manufacturer's service publications. The student will locate information in the reference publications and describe the checking and servicing of a fuel dump system. Correct nomenclature and terminology will be used as a part of the description of operation. 42. Perform fuel management transfer and defueling (EIT = 2 hrs, T = 2 hrs, L/S = 0 hrs) Level 1 A. Perform fuel transfer and defueling Level 1 Schematic diagrams or mock-ups of a fuel system that incorporates provisions for cross feed, fuel transfer and the service publications associated with the specific system. The student will locate information in the appropriate technical publication and describe the procedures necessary to transfer or cross feed fuel and defuel the system. Correct nomenclature and terminology will be used as a part of the description of operation. IV /01/ /01/2016

40 43. Inspect, check, and repair pressure fueling systems (EIT = 2 hrs, T = 2 hrs, L/S = 0 hrs) Level 1 A. Describe the inspection, checking and repair of pressure fueling systems Level 1 Visual aids, mock-ups and technical data as would be available from the manufacturer's service manual. The student will describe the procedures to be followed when inspecting, checking and repairing pressure type fueling systems, Standards: Reference publications will be used during the descriptions. Correct nomenclature and terminology is required as a part of the descriptions. 44. Repair aircraft fuel system components (EIT = 10 hrs, T = 5 hrs, L/S = 5 hrs) Level 2 A. Interpret information pertaining to repair of fuel system components Level 2 Typical aircraft fuel tanks of the separate metal types, flexible bladder types and integral type; fuel strainers, selector valves, fuel lines of the solid metal and flexible hose types, fuel drains, appropriate reference information, and ten written questions pertaining to repair of fuel system components. The student will locate and interpret information from the manuals and describe the repair procedures for fuel system components as specified in the ten written questions. The repair procedures will be interpreted without error. Correct nomenclature and terminology will be used as a part of all descriptions. IV /01/ /01/2016

41 45. Inspect and repair fluid quantity indicating systems (EIT = 6 hrs, T = 3 hrs, L/S = 3 hrs) Level 2 A. Inspect and troubleshoot fuel quantity indication systems Level 2 An operational fuel quantity indicating system of the direct reading (sight gauge or Mechanical float) and a remote indicating electrical type; appropriate reference information and ten statements describing malfunctions of "the systems. The student will inspect the operating systems, correctly interpret information from the manuals and describe the repair that would be undertaken to correct the malfunctions described in the ten statements. The repair practices and recommendations of the manual will be interpreted without error. Correct nomenclature will be used as part of all described repairs. 46. Troubleshoot, service, and repair fluid pressure and temperature warning systems (EIT = 2 hrs, T = 1 hr, L/S = 1 hr) Level 2 A. Troubleshoot, service, and repair fuel pressure and temperature warning systems Level 2 An operating fuel system installed in an airplane or on a mockup, including a pressure and temperature warning system, a schematic or diagram of the system and the service information applicable to the specific system. The student will operate the system and adjust the pressure or temperature sensing devices. He will interpret information from the ser«vice information and identify the cause of an instructorintroduced fault in the system. He will repair the system as directed in the service manual. IV /01/ /01/2016